Concentrated Photovoltaic System Modules Using III-V Semiconductor Solar Cells

ABSTRACT

A solar cell receiver for use in a concentrating solar system which concentrates the solar energy onto a solar cell for converting solar energy to electricity. The solar cell receiver may include a solar cell mounted on a support and with one or more III-V compound semiconductor layers. An optical element may be positioned over the solar cell and have an optical channel with an inlet that faces away from the solar cell and an outlet that faces towards the solar cell. A frame may be positioned over the support and extend around the solar cell with the frame having an inner side that extends above the support and faces towards the optical element. An encapsulant may be positioned over the support and contained between the optical element and the frame. The encapsulant may have enlarged heights at contact points with the optical element and the frame and a reduced height between the contact points away from the optical element and the frame. The solar cell receiver may be used in a solar cell module.

RELATED APPLICATIONS

The present application is a continuation-in-part of U.S. patent application Ser. No. 12/582,047 filed Oct. 20, 2009, which itself is a continuation-in-part of U.S. patent application Ser. No. 12/069,642 filed Feb. 11, 2008, the contents of which are herein incorporated by reference in their entirety.

The disclosure of this application is related to U.S. application Ser. No. 12/764,657 filed on Apr. 21, 2010 which is a continuation-in-part of U.S. application Ser. No. 12/553,813 filed on Sep. 3, 2009; U.S. application Ser. No. 12/485,684, filed on Jun. 16, 2009; U.S. application Ser. No. 12/246,295, filed on Oct. 6, 2008; U.S. application Ser. No. 12/264,369, filed on Nov. 4, 2008 which is a divisional of Ser. No. 12/069,642; U.S. application Ser. No. 11/849,033, filed on Aug. 31, 2007; U.S. application Ser. No. 11/830,576, filed on Jul. 30, 2007; and U.S. application Ser. No. 11/500,053, filed on Aug. 7, 2006, the contents of which are incorporated herein by reference in their entirety.

BACKGROUND

Satisfying the world's growing demand for energy is one of the most significant challenges facing society. At present, about 85% of the energy produced in the United States comes from fossil fuels. Given that the supply of such fuels is on the decline, their prices continue to rise, and the resultant greenhouse gases may contribute to global warming, there is a need to develop new technologies that are economically feasible and environmentally friendly.

Solar energy is one technology for power generation that is clean, quiet and renewable. It is also plentiful: with an average of roughly 125,000 terawatts of solar energy reaching the planet at any given time, solar technology can potentially generate a significant amount of energy.

Solar cells are used to convert solar or radiant energy into electricity. Historically, solar power (both in space and terrestrially) has been predominantly provided by silicon solar cells. In the past several years, however, high-volume manufacturing of high-efficiency III-V multijunction solar cells has enabled the consideration of this alternative technology for terrestrial power generation. Compared to Si, III-V multijunction cells are generally more radiation resistant and have greater energy conversion efficiencies, but they tend to cost more. Some current III-V multijunction cells have energy efficiencies that exceed 27%, whereas silicon technologies generally reach only about 17% efficiency. Under concentration, some current III-V multijunction cells have energy efficiencies that exceed 37%. When the need for very high power or smaller solar arrays are paramount in a spacecraft or other solar energy system, multijunction cells are often used instead of, or in hybrid combinations with, Si-based cells to reduce the array size.

Generally speaking, the multijunction cells are of n-on-p polarity and are composed of InGaP/(In)GaAs/Ge compounds. III-V compound semiconductor multijunction solar cell layers can be grown via metal-organic chemical vapor deposition (MOCVD) on Ge substrates. The use of the Ge substrate permits a junction to be formed between n- and p—Ge. The solar cell structures can be grown on 100-mm diameter (4 inch) Ge substrates with an average mass density of about 86 mg/cm^(2.)

In some multijunction cells, the middle cell is an InGaAs cell as opposed to a GaAs cell. The indium concentration may be in the range of about 1.5% for the InGaAs middle cell. In some implementations, such an arrangement exhibits increased efficiency. The InGaAs layers are substantially perfectly lattice matched to the Ge substrate.

Regardless of the type of cell used, a known problem with solar energy systems is that individual solar cells can become damaged or shadowed by an obstruction. For example, damage can occur as a result of exposure of a solar cell to harsh environmental conditions. The current-carrying capacity of a panel having one or more damaged or shadowed solar cells is reduced, and the output from other panels in series with that panel reverse biases the damaged or shadowed cells. The voltage across the damaged or shadowed cells thus increases in a reverse polarity until the full output voltage of all of the panels in the series is applied to the damaged or shadowed cells in the panel concerned. This causes the damaged or shadowed cells to break down.

As a solar cell system for terrestrial applications has thousands of solar cells, its voltage output is normally in the range of hundreds of volts, and its current output is in the range of tens of amperes. At these output power levels, if the solar cell terminals are not protected, uncontrollable electric discharge in the form of sparks tends to occur, and this can cause damage to the solar cells and to the entire system.

The multijunction solar cell forms part of a solar cell receiver that may be used in the concentrator solar cell system. The solar cell receivers may be used in environments where water, extreme heat, and humidity may erode performance and/or cause failure. Standards and testing qualifications have been instituted to ensure that a solar cell receiver meets minimum requirements during use. One specific industry standard is IEC62108. Solar cell receivers should be constructed in a manner to meet the requirements of these standards to ensure proper performance.

SUMMARY

The present application is directed to a solar cell module to convert light to electricity. The solar cell module may include a housing with a plurality of lenses that form an enclosed interior space. The solar cell module may also include a plurality of solar cell receivers connected to the housing and spaced away from the plurality of lenses. Each of the solar cell receivers may include: a ceramic substrate with a first metalized surface and an opposing second metalized surface with the first metalized surface having separate conductive regions; a III-V compound semiconductor multijunction solar cell having an anode terminal electrically connected to a first one of the conductive regions of the ceramic substrate and a cathode terminal electrically connected to a second one of the conductive regions; a bypass diode connected across the first and second conductive regions of the ceramic substrate in parallel with the solar cell; a first optical element positioned above the solar cell and including a tapered shape with a larger inlet that faces away from the solar cell and a smaller outlet that faces towards the solar cell; and a second optical element positioned above the solar cell. The solar cell module may also include a frame positioned over the ceramic substrate and having a height above the ceramic substrate that is greater than the solar cell. The frame may extend around and enclose the solar cell in an interior space. The solar cell module may also include an encapsulant contained within the interior space between the second optical element and the frame and covering portions of the ceramic substrate and the solar cell. The encapsulant may have an enlarged fillet height at each of the second optical element and the frame. Each of said solar cell receivers, first optical elements, and second optical elements may be disposed in an optical path of one of the plurality of lenses with the lens, the first optical element, and the second optical element concentrating the light onto the respective solar cell by a factor of 1000 or more to generate in excess of 25 watts of peak power.

The present application is also directed to various solar cell receivers. The solar cell receiver may include a solar cell mounted on a support and including one or more III-V compound semiconductor layers. An optical element may be positioned over the solar cell on an opposite side from the support. The optical element may define an optical channel and include an enlarged inlet that faces away from the solar cell and a reduced outlet that faces towards the solar cell. A frame may be positioned over the support and have a height above the support that is greater than the solar cell. The frame may extend around and enclose the solar cell in an interior space. An encapsulant may be contained within the interior space between the optical element and the frame and cover portions of the support and the solar cell. The encapsulant may have an enlarged fillet height at each of the optical element and the frame.

The solar cell receiver may also include a solar cell mounted on a support and having one or more III-V compound semiconductor layers. An optical element may be positioned over the solar cell and have an optical channel with an inlet that faces away from the solar cell and an outlet that faces towards the solar cell. A frame may be positioned over the support and extend around the solar cell. The frame may have an inner side that extends above the support and faces towards the optical element with the inner side being positioned between 2.0 mm to 5.0 mm away from the optical element. An encapsulant may be positioned over the support and contained between the optical element and the frame. The encapsulant may have a minimum thickness of 0.5 mm to 2.0 mm with enlarged heights at contact points with the optical element and the frame of between about 1.0 mm to 3.0 mm and a reduced height between the contact points away from the optical element and the frame.

The present application also includes a method of making a solar cell receiver. The method may include mounting a solar cell on a support with the solar cell comprising one or more III-V compound semiconductor layers. The method may including mounting bond wires between the solar cell and the support and mounting an optical element defining an optical channel over the solar cell so that the solar cell is in the optical path of the optical channel. The method may include mounting a frame on the support that surrounds the solar cell and defines an enclosed interior space between the frame and the optical element. The method may include introducing a fluid encapsulant in the enclosed interior space between the frame and the optical element and encapsulating at least a portion of the solar cell, the bond wires, and at least a portion of the optical element. The fluid encapsulant may have an increased surface tension and may form enlarged fillets at the optical element and the frame and a reduced intermediate section with the fillets having a greater height above the support than the intermediate section. The method may also include curing the fluid encapsulant.

Of course, the present invention is not limited to the above features and advantages. Those skilled in the art will recognize additional features and advantages upon reading the following detailed description, and upon viewing the accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

The present invention will be now described more fully hereinafter with reference to the accompanying drawings, in which some, but not all embodiments of the invention are shown. Drawings illustrating the embodiments are not-to-scale schematic representations. For the purpose of the present description and of the appended claims, all ranges include the maximum and minimum points disclosed and include any intermediate ranges therein, which may or may not be specifically enumerated herein.

FIG. 1 is a perspective view of an implementation of a solar cell module.

FIG. 2 is a perspective view of an implementation of a secondary optical element.

FIG. 3 is a partially exploded perspective view of an implementation of a solar cell receiver.

FIG. 4 is a partially exploded perspective view illustrating the solar cell and the metalized ceramic substrate of FIG. 3 in more detail.

FIG. 5 is a sectional view of the solar cell, the metalized ceramic substrate and the heat sink along line X-X′ of FIG. 3.

FIG. 6 is a perspective view of a solar cell receiver with a frame and encapsulant.

FIG. 7 is a cross-sectional view cut along line Y-Y′ of FIG. 6.

FIG. 8 is a cross-sectional view of encapsulant positioned within a frame.

FIG. 9 is a cross-sectional view of encapsulant positioned within a frame.

FIG. 10 is a cross-sectional view of encapsulant positioned within a frame.

DETAILED DESCRIPTION

FIG. 1 illustrates an implementation of a solar cell module 200 comprising an array of lenses 210 and corresponding solar cell receivers 100. Each one of the lenses 210 is aligned with one of the solar cell receivers 100. The solar cell module 200 may include various numbers of lenses 210 and solar cell receivers 100. FIG. 1 includes a module 200 with fifteen lenses 210 and solar cell receivers 100 aligned in a 3×5 array.

The lenses 210 are formed on a continuous sheet 211 of optical material (e.g., acrylic). In some implementations, regions of the sheet 211 not formed into the lenses 210 are made partially or entirely opaque. By forming the lenses 210 out of a continuous sheet 211, costs can be decreased substantially. First, by producing the lenses 210 on large sheets, production costs are decreased. Second, assembly costs are decreased because only one item (i.e., the sheet 211 of lenses) needs to be aligned with the solar cell receivers 100. In this implementation, the sheet 211 lies atop an alignment frame 221 of a housing 220.

One or more vent openings 228 may be positioned in the housing 220. The openings 228 may be positioned to facilitate air flow through the housing 220. In one embodiment, the openings 228 are positioned in the sidewalls of the housing 220 and about 3″ below the lenses 210. The size of the openings 228 may vary. In one embodiment, each opening has a circular shape with a diameter of about 1″. A cover 229 may extend across the openings 228 and act as a filter to impede the introduction of moisture and debris into the housing 220. The cover 229 may be constructed of a variety of materials, including but not limited to GORETEX, nylon, and polyvinylidene.

The frame 221 may include a plurality of frame alignment elements, such as holes. The alignment elements may be threaded or otherwise adapted to receive a fastener. The sheet 211 may include sheet alignment elements such as pins, screws or other hardware that align and couple with the frame alignment elements. The frame alignment elements and the sheet alignment elements are located such that by coupling the sheet alignment elements with the frame alignment elements, each of the lenses 210 is aligned with a corresponding solar cell receiver 100. The alignment elements are located generally in a center point defined by four of the lenses 210. In one embodiment, an alignment element is located in a center point defined by lenses 210 a, 210 b, 210 c, and 210 d. Another alignment element may be located in a center point defined by four other lenses 210. This pattern of locating the alignment elements in a center point defined by four lenses can continue along the entire sheet 211.

In some implementations, the floor surface 222 of the housing 220 comprises alignment features that ensure that each of the solar cell receivers 100 is located in a predetermined position. These features may couple with each of the solar cell receivers 100.

In some implementations, each of the lenses 210 is a Fresnel lens. The corresponding solar cell receiver 100 is positioned on the surface 222 at an opposite end of the housing 220. Each of the solar cell receivers 100 includes a corresponding solar cell 102 disposed in the optical path of the corresponding lens 210, i.e., such that the corresponding solar cell 102 receives light that passes through the corresponding lens 210. In some implementations, additional optical elements are employed to place the solar cell in the optical path of the lens. For example, secondary optical elements 104 correspond with each pair of the solar cell receivers 100 and the lenses 210. The secondary optical elements 104 gather the light from the lens 210 and direct it into the solar cell 102 of the solar cell receiver 100. In some implementations, each of the solar cell receivers 100 is provided with a corresponding secondary optical element 104.

Another optical element includes a concentrator 106 that is positioned between each of the pairs of solar cell receivers 100 and lenses 210. The concentrator 106 concentrates the light onto the solar cell 102.

While some Fresnel lenses can concentrate more sunlight than some convex lenses, implementations may use any type of lens 210 that concentrates the incident sunlight. For example, any of lenses 210 may take the form of a biconvex lens, a plano-convex lens, or a convex-concave lens. The lenses 210 may also comprise a multi-layer anti-reflective coating. In a module 200, each of the lenses 210 may be the same, or the module 200 may include two or more different lenses 210.

A distance X measured between the sheet 211 comprising the lenses 210 and the solar cells 102 of the corresponding solar cell receivers 100 may be chosen based on the focal length of the lenses 210. In some implementations the housing 220 is arranged so that the solar cell 102 of each respective solar cell receiver 100 is disposed at or about the focal point of the respective lens 210. In some implementations, the focal length of each of the lenses 210 is between about 25.4 cm (10 inches) and 76.2 cm (30 inches). In some implementations, the focal length of each lens 210 is between about 38.1 cm (15 inches) and 50.8 cm (20 inches). In some implementations, the focal length of each lens 210 is about 40.085 cm (17.75 inches). In some implementations, the focal length of each lens 210 varies, and the housing 220 provides multiple different distances (e.g., those that are greater and/or lesser than the distance X) between the sheet 211 and the surface 222.

The housing 220 and the lens sheet 211 may form an enclosed interior space that protects the solar cell receivers 100 from the environment.

Some implementations of the lenses 210 concentrate incident sunlight to 1000 times normal concentration (i.e., 1000 Suns) or more. Other implementations may include other concentrations. Generally speaking, conversion efficiency of solar energy into electricity increases under concentrated illumination. For example, at about 1000 Suns, a single solar cell receiver can generate 25 watts or more of electrical power. In another example, at about 470 Suns or more, a single solar cell receiver can generate 14 watts or more of electrical power. The amount of electrical power a solar cell receiver can produce can vary depending on, for example, the combination of solar cell characteristics (e.g., size, composition) and properties of the associated optics (e.g., concentration, focus, alignment).

In some implementations, the solar cells 102 of each of the respective solar cell receivers 100 is a triple-junction III-V solar cell, with each of the three subcells arranged in series. In applications where multiple solar cell modules 200 are employed, the receivers 100 of the solar cell modules 200 are typically electrically connected together in series. However, other applications may utilize parallel or series-parallel connection. For example, receivers 100 within a given module 200 can be electrically connected together in series, but the modules 200 are connected to each other in parallel.

As previously explained, a secondary optical element (“SOE”) 104 may be positioned between the lens 210 and the corresponding solar cell 102. An implementation of an SOE is illustrated in FIG. 2. The SOE 104 is disposed inside the housing 220 of the solar cell module 200 and is generally designed to collect solar energy concentrated by one of the corresponding lenses 210. In some implementations, each of the solar cell receivers 100 has a respective SOE 104. Other modules 200 may include less than each solar cell receiver 100 including an SOE 104.

The SOE 104 comprises an optical element 401 with an optical inlet 402 and an optical outlet 403, a body 404 and mounting tabs 405. The SOE 104 is mounted such that the optical element 401 is disposed above the solar cell 102 of the corresponding solar cell receiver 100. While it may vary depending on the implementation, the SOE 104 is mounted such that the optical outlet 403 is about 0.5 millimeters from the solar cell 102 (e.g., dimension 406 is about 0.5 millimeters). In some implementations, mounting tabs 405 couple to the surface 222 of the housing 220. The SOE 104 may be made of metal, plastic, or glass or other materials.

In some implementations, the optical element 401 has a generally square cross section that tapers from the inlet 402 to the outlet 403. The inside surface 407 of the optical element reflects light downward toward the outlet 403. The inside surface 407 is, in some implementations, coated with silver or another material for high reflectivity. In some cases, the reflective coating is protected by a passivation coating such as SiO₂ to protect against oxidation, tarnish or corrosion. The path from the optical inlet 402 to the optical outlet 403 forms a tapered optical channel that catches solar energy from the corresponding lens 210 and guides it to the corresponding solar cell 102. As shown in this implementation, the SOE 104 comprises an optical element 401 having four reflective walls. In other implementations, different shapes (e.g., three-sided to form a triangular cross-section) may be employed.

Under ideal conditions, the corresponding lens 210 associated with the SOE 104 focuses the light directly to the solar cell 102 without the light hitting against the SOE 104. In most circumstances, the lens 210 does not focus light directly on the solar cell 102. This may occur due to a variety of causes, including but not limited to chromatic aberration of a refractive lens design, misalignment of the solar cell 102 relative to the lens 210 during construction, misalignment during operation due to tracker error, structural flexing, and wind load. Thus, under most conditions, the lens 210 focuses the light such that it reflects off the SOE 104. The difference between an ideal setup and a misaligned setup may be a minor variation in the positioning of the lens 210 of less than 1°. The SOE 104 therefore acts as a light spill catcher to cause more of the light to reach the solar cell 102 in circumstances when the corresponding lens 210 does not focus light directly on the solar cell 102. The SOE 104 can include a reflective multi-layer intermediate region such as the kind disclosed in U.S. patent application Ser. No. 12/402,814 filed on Mar. 12, 2009, which is incorporated herein by reference in its entirety.

The reflective multi-layer intermediate region can be formed from different materials and have different optical characteristics so that the reflectivity of the light beams off the SOE 104 and transmitted to the solar cell 102 optimizes the aggregate irradiance on the surface of the solar cell 102 over the incident solar spectrum. For example, in some implementations, the inner surface 407 can be coated with silver or another material for high reflectivity. In some cases, the reflective coating is protected by a passivation coating such as SiO₂ to protect the SOE 104 against oxidation, tarnish or corrosion. The SOE 104 may also homogenize (e.g., mix) the light. In some cases, it also has some concentration effect.

In some implementations, the optical inlet 402 is square-shaped and is about 49.60 mm×49.60 mm (dimension 408), the optical outlet is square-shaped and is about 9.9 mm×9.9 mm (dimension 409) and the height of the optical element is about 70.104 mm (dimension 410). The dimensions 408, 409, and 410 may vary with the design of the solar cell module 200 and the solar cell receiver 100. For example, in some implementations the dimensions of the optical outlet 403 are approximately the same as the dimensions of the solar cell 102. For an SOE 104 having these dimensions, the half inclination angle is 15.8 degrees.

Each of the solar cells 102 may be a triple-junction III-V compound semiconductor solar cell which comprises a top cell, a middle cell and a bottom cell arranged in series. In another embodiment, the solar cells 102 are multijunction solar cells having n-on-p polarity and is composed of InGaP/(In)GaAs III-V compounds on a Ge substrate. In each case, the solar cells 102 are positioned to receive focused solar energy from SOE 104 and/or the corresponding lens 210.

An anti-reflective coating may be disposed on the solar cell 102. The anti-reflective coating may be a multi-layer antireflective coating providing low reflectance over a certain wavelength range, e.g., 0.3 to 1.8 μm. An example of an anti-reflective coating is a dual-layer TiO_(x)/Al₂O₃ dielectric stack.

As illustrated in FIG. 3, the tabs 405 of the SOE 104 may be configured for attaching the SOE 104 to a bracket 116 via one or more fasteners 118. The bracket 116 is provided for mounting the SOE 104 to a heat sink 120 via one or more fasteners 122. The bracket 116 is thermally conductive so that heat energy generated by the SOE 104 during operation can be transferred to the heat sink 120 and dissipated.

In one embodiment as shown in FIGS. 3 and 4, a concentrator 106 is disposed between the outlet 403 of the SOE 104 and the solar cell 102. The concentrator 106 is preferably glass and has an optical inlet 108 and an optical outlet 110. In one embodiment, the concentrator 106 is solid glass. The concentrator 106 amplifies the light exiting the SOE 104 and directs the amplified light toward the solar cell 102. In some implementations, the concentrator 106 has a generally square cross section that tapers from the inlet 108 to the outlet 110. In some implementations, the optical inlet 108 of the concentrator 106 is square-shaped and is about 2 cm×2 cm and the optical outlet 110 is about 0.9 cm×0.9 cm. The dimensions of the concentrator 106 may vary with the design of the solar cell module 200 and the solar cell receiver 100. For example, in some implementations the dimensions of the optical outlet 110 are approximately the same as the dimensions of the solar cell 102. In one embodiment, the concentrator 106 is a 2× concentrator. The bottom surface of the concentrator 106 can be directly attached to the upper surface of the solar cell 102 using an adhesive 151 such as a silicone adhesive. The solar cell 102 converts the incoming sunlight directly into electricity by the photovoltaic effect.

In some embodiments as illustrated in FIGS. 1 and 3, both an SOE 104 and a concentrator 106 are positioned along the optical path between the corresponding lens 210 and solar cell 102. Other embodiments may include just one of these optical elements positioned along the optical path. Other embodiments may include neither of these elements along the optical path. Within a module 200, each of the lens 210/solar cell 102 pairs may include the same or different combination of elements for directing the light.

As illustrated in FIGS. 3 and 4, a bypass diode 124 is connected in parallel with the solar cell 102. In some implementations, the diode 124 is a semiconductor device such as a Schottky bypass diode or an epitaxially grown p-n junction. For purposes of illustration, the bypass diode 124 is a Schottky bypass diode. External connection terminals 125 and 127 are provided for connecting the solar cell 102 and the diode 124 to other devices, e.g., adjacent solar cell receivers (not illustrated).

The functionality of the bypass diode 124 can be appreciated by considering multiple solar cells 102 connected in series. Each solar cell 102 can be envisioned as a battery, with the cathode of each of the diodes 124 being connected to the positive terminal of the associated “battery” and the anode of each of the diodes 124 being connected to the negative terminal of the associated “battery.” When one of the serially-connected solar cell receivers 100 becomes damaged or shadowed, its voltage output is reduced or eliminated (e.g., to below a threshold voltage associated with the diode 124). Therefore, the associated diode 124 becomes forward-biased, and a bypass current flows only through that diode 124 (and not the solar cell 102). In this manner, the non-damaged or non-shadowed solar cell receivers 100 continue to generate electricity from the solar energy received by those solar cells. If not for the bypass diode 124, substantially all of the electricity produced by the other solar cell receivers would pass through the shadowed or damaged solar cell receiver, destroying it, and creating an open circuit within, e.g., the panel or array.

The solar cell receiver 100 also includes a ceramic substrate 126 such as an alumina substrate for mounting of the solar cell 102 and the heat sink 120 for dissipating heat generated by the solar cell 102 during operation. FIGS. 4 and 5 illustrate the solar cell 102 and the ceramic substrate 126 in more detail. The ceramic substrate 126 has metalized upper and lower surfaces 128 and 130. Both surfaces 128 and 130 of the ceramic substrate 126 are metalized to increase the heat transfer capacity of the ceramic substrate 126, enabling the solar cell receiver 100 to more adequately handle rapid temperature changes that occur due to abrupt changes in solar cell operating conditions. For example, the solar cell 102 generates heat energy when converting light to electricity. Having both the upper and lower surfaces 128 and 130 of the ceramic substrate 126 metalized provides for a faster transfer of the heat energy from the solar cell 102 to the heat sink 120 for dissipation. The opposite condition occurs when the solar cell 102 becomes suddenly shaded. That is, the solar cell 102 stops producing electricity and rapidly cools as does the SOE 104. The metalized upper and lower surfaces 128 and 130 of the ceramic substrate 126 prevent the solar cell 102 from cooling too rapidly by transferring heat energy from the heat sink 120 to the solar cell 102, and depending on the thermal conditions, to the SOE 104 as well. The increased heat transfer capacity of the solar cell receiver 100 reduces the amount of stress imparted to the interface between the solar cell 102 and the ceramic substrate 126 during rapid temperature changes, ensuring a reliable solar cell-to-substrate interface.

The metalized upper surface 128 of the ceramic substrate 126 is in contact with the solar cell 102 and has separated conductive regions 132 and 134 for providing isolated electrically conductive paths to the solar cell 102. The first conductive region 132 provides an anode electrical contact point for the solar cell 102 and the second conductive region 134 provides a cathode electrical contact point for the solar cell 102. The solar cell 102 has a conductive lower surface 130 out-of-view in FIG. 4, but visible in the cross-section of FIG. 5 that is positioned on and connected to the first conductive region 132 of the metalized upper surface 128 of the ceramic substrate 126. The opposing upper surface 138 of the solar cell 102 has a conductive contact area 140 connected to the second conductive region 134 of the ceramic substrate 126.

In one embodiment, the conductive lower surface 136 of the solar cell 102 forms an anode terminal of the solar cell 102 and the conductive contact area 140 disposed at the upper surface 138 of the solar cell 102 forms a cathode terminal. According to this embodiment, the conductive lower surface 136 of the solar cell 102 is positioned on the first conductive region 132 of the ceramic substrate 126 and electrically isolated from the second conductive region 134 to ensure proper operation of the solar cell 102. In one embodiment, the first conductive region 132 of the ceramic substrate 126 is at least partly surrounded on three sides by the second conductive region 134 about a periphery region of the ceramic substrate 126.

In one embodiment, the conductive contact area 140 disposed at the upper surface 138 of the solar cell 102 occupies the perimeter of the solar cell 102. In some implementations, the upper conductive contact area 140 can be smaller or larger to accommodate the desired connection type. For example, the upper conductive contact area 140 may touch only one, two or three sides (or portions thereof) of the solar cell 102. In some implementations, the upper conductive contact area 140 is made as small as possible to maximize the area that converts solar energy into electricity, while still allowing electrical connection. While the particular dimensions of the solar cell 102 will vary depending on the application, standard dimensions are about a 1 cm². For example, a standard set of dimensions can be about 12.58 mm×12.58 mm overall, about 0.160 mm thick, and a total active area of about 108 mm². For example, in a solar cell 102 that is approximately 12.58 mm×12.58 mm, the upper conductive contact area 140 can be about 0.98 mm wide and the active area can be about 10 mm×10 mm.

The upper conductive contact area 140 of the solar cell 102 may be formed of a variety of conductive materials, e.g., copper, silver, and/or gold-coated silver. In this implementation, it is the n-conductivity cathode (i.e. emitter) side of the solar cell 102 that receives light, and accordingly, the upper conductive contact area 140 is disposed on the cathode side of the solar cell 102. In one embodiment, the upper conductive contact area 140 of the solar cell 102 is wire bonded to the second conductive region 134 of the metalized upper surface 128 of the ceramic substrate 126 via one or more bonding wires 142. The number of bonding wires 142 utilized in a particular implementation can be related, among other things, to the amount of current generated by the solar cell 102. Generally, the greater the current, the greater number of bonding wires 142 that are used.

The bypass diode 124 couples the first conductive region 132 of the metalized upper surface 128 of the ceramic substrate 126 to the second conductive region 134. In one embodiment, a cathode terminal of the bypass diode 124 is connected to the anode terminal of the solar cell 102 via the first conductive region 132 of the ceramic substrate 126 and an anode terminal of the bypass diode 124 is electrically connected to the cathode terminal of the solar cell 102 via the second conductive region 134 of the ceramic substrate 126. The anode terminal of the solar cell 102 is formed by the lower conductive surface 136 of the solar cell 102 as described above and is out-of-view in FIG. 4, but visible in the cross-section of FIG. 5. The cathode terminal of the solar cell 102 is formed by the upper conductive contact area 140 of the solar cell 102 also as described above.

The external connection terminals 125, 127 disposed on the metalized upper surface 128 of the ceramic substrate 126 provide for electrical coupling of a device to the solar cell 102 and the bypass diode 124. In some implementations, the connector terminals 125 and 127 correspond to anode and cathode terminals, and are designed to accept receptacle plugs (not shown) for connection to adjacent solar cell receivers.

The upper surface 128 of the ceramic substrate 126 can be metalized by attaching metallization layers 132 and 134 to the substrate. In one embodiment, holes 144 are formed in the metallization layers 132, 134. FIG. 4 shows the ceramic substrate 126 having two metallization layers 132 and 134 attached to the upper substrate surface 128 (the lower metalized surface is out of view in FIG. 4, but visible in the cross-section of FIG. 5). Corresponding bumps can be formed on the ceramic substrate 102. The bumps are at least partly seated in the holes 144 formed in the metallization layers 132 and 134. The holes 144 in the metallization layers 132 and 134 are then filled with a solder or other type of bonding material such as an adhesive, attaching the metallization layers 132 and 134 to the upper surface 128 of the ceramic substrate 126. The lower surface 130 of the ceramic substrate 126 can be similarly metalized. Alternatively, no bumps are provided on the ceramic substrate 126 and the substrate is relatively planar within normal manufacturing tolerances.

FIG. 5 illustrates a cross-sectional view of the solar cell 102, ceramic substrate 126 and heat sink 120 of the solar cell receiver 100 along the line labeled X-X′ in FIG. 3. The SOE 104, light concentrator 106 and terminals 125, 127 are not illustrated in FIG. 5 for ease of illustration. The upper and lower surfaces 128 and 130 of the ceramic substrate 126 may have bumps that are at least partly seated in holes 144 formed in metallization layers 132, 134 and 148 for attaching the metallization layers to the ceramic substrate 126 as described above. Alternatively, the ceramic substrate 126 is relatively flat within normal manufacturing tolerances. In either case, the upper and lower surfaces of the ceramic substrate 126 are metalized. The upper metalized surface 128 of the substrate 126 has separated conductive regions 132 and 134 for providing electrically isolated anode and cathode connections to the solar cell 102 as described above.

The solar cell 102 has a conductive lower surface 136 connected to the conductive region 132 of the metalized upper surface 128 of the ceramic substrate 126. In one embodiment, the conductive lower surface 136 of the solar cell 102 forms the anode terminal of the solar cell 102 and the conductive contact area 140 disposed at the upper surface 138 of the solar cell 102 forms the cathode terminal of the solar cell 102. The conductive lower surface 136 of the solar cell 102 is positioned on the first conductive region 132 of the metalized upper surface 128 of the ceramic substrate 126 and electrically isolated from the second conductive region 134 to ensure proper operation of the solar cell 102.

The lower surface 130 of the ceramic substrate 126 also has a metallization layer 148 that is bonded to the heat sink 120 with a highly thermally conductive attach media 150, such as a metal-filled epoxy adhesive or solder. Filling an epoxy adhesive such as silicone with metal increases the thermal conductivity of the interface between the ceramic substrate 126 and the heat sink 120, further improving the heat transfer characteristics of the solar cell receiver 100. In one embodiment, the highly thermally conductive attach media 150 is a metal-filled epoxy adhesive having a thickness t_(epoxy) of approximately 1 to 3 mils. The metal-filled epoxy adhesive can be applied to the lower metalized surface 130 of the ceramic substrate 126, the heat sink 120 or both and then cured to bond the heat sink 120 to the substrate 126. In one embodiment, the heat sink 120 is a single-piece extruded aluminum heat sink as shown in FIG. 3.

The solar cell receiver 100 can be manufactured by providing the metalized ceramic substrate 126 and connecting the conductive lower surface 136 of the solar cell 102 to the first conductive region 132 of the metalized upper surface 128 of the substrate 126. The conductive contact area 140 disposed at the upper surface 138 of the solar cell 102 is connected to the second conductive region 134 of the metalized upper surface 128 of the ceramic substrate 126, e.g. via one or more bonding wires 142. The heat sink 120 is bonded to the lower metalized surface 130 of the ceramic substrate 126 with the metal-filled epoxy adhesive 150.

As illustrated in FIG. 6, a frame 170 may be attached to the metallic surface 128 of the ceramic substrate 126 and extend around the solar cell 102 and related components. The frame 170 includes an open central region 174 and forms a dam for an encapsulant 160 that covers a portion of the solar cell receiver 100. The encapsulant 160 protects the solar cell receiver 100 from environmental elements such as water (e.g., rain, ice, snow) temperature variations, and humidity. The frame 170 may also form a shield for providing off-axis beam protection and for sealing the connection terminals 125, 127.

The frame 170 may include various cross-sectional shapes when viewed in a plane that extends through the bottom and top sides 172, 173. FIG. 7 includes a rectangular shape with opposing inner and outer sides 171, 177, and opposing bottom and top sides 172, 173. Frame 170 may also include a variety of other cross-sectional shapes depending upon the application. In one specific embodiment, the frame 170 includes an irregular shape.

The frame 170 may be solid as illustrated in FIG. 7, or may be hollow with an open interior space 178 as illustrated in FIG. 9. FIG. 9 includes the frame 170 completely surrounding the interior space 178. In another embodiment (not illustrated), the frame 170 surrounds basically three sides of the interior space 178 with the interior space 178 being exposed on the bottom side (i.e., opposite from the top side 173).

Frame 170 may be constructed from one or more pieces. In one embodiment, the frame 170 is constructed from two substantially L-shaped pieces. The exterior and interior shapes of the frame 170 may vary depending upon the application. The exterior shape is formed by the outer sides 177 of the frame 170, and the interior shape is formed by the inner sides 171. FIG. 6 includes a frame 170 with square interior and exterior shapes. The interior and exterior shapes may also include but are not limited to rectangular, circular, oval, and trapezoidal. Further, the interior and exterior shapes may be the same or may be different. The frame 170 may be constructed from a variety of materials, including ceramic.

FIG. 7 illustrates a cross-section view of the encapsulant 160 positioned within the frame 170 and over a portion of the solar cell receiver 100. The encapsulant 160 extends over a portion of the concentrator 106, the metalized upper surface 128 of the ceramic substrate 126, portions of the solar cell 102 including the contact area 140, and the bonding wires 142 that extend between the contact area 140 and the metalized upper surface 128. The encapsulant 160 is prevented from extending between the concentrator 106 and the solar cell 102 by a light transparent adhesive 151 that bonds the concentrator 106 to the solar cell 102.

The encapsulant 160 is initially in a fluid form to flow into the various areas within the frame 170. The encapsulant 160 further cures to a more solid state to permanently protect the solar cell receiver 100. In one embodiment, the encapsulant 160 is SYLGARD 184 available from Dow Corning Corporation.

FIG. 8 is a simplified sectional view similar to FIG. 7 that illustrates the dimensions and positioning of the frame 170 and the encapsulant 160. The frame 170 includes a height a measured between a bottom side 172 and a top side 173. The height “a” provides for the top side 173 to be positioned along an intermediate section of the concentrator 106 and extend outward from the upper metallic surface 128 a greater distance than the bottom side 109 of the concentrator 106. An inner side 171 of the frame 170 faces towards the concentrator 106 and may be flat and aligned substantially perpendicular to the upper metallic surface 128. The inner side 171 is positioned a distance “b” from the intersection of the bottom and intermediate sides 109, 111 of the concentrator 106. In some embodiments, the distance b may be between 2.0 mm to 5.0 mm.

The distance between the frame 170 and concentrator 106 and the physical characteristics of the encapsulant 160 causes a high surface tension in the encapsulant 160 when placed within the interior space 178. This causes the encapsulant 160 to climb the intermediate side 111 of the concentrator 106 and the inner side 171 of the frame 170. This gives the encapsulant 160 a substantially concave upper surface with enlarged inner and outer fillets 161, 162 and a reduced intermediate section 163. The height of the inner and outer fillets 161, 162 measured from the upper metallic surface 128 is between about 1.0 mm and 3.0 mm. In several specific embodiments, the heights are between about 1.75 mm and 1.90 mm. The heights of the encapsulant 160 may be different at the inner fillet 161 than at the outer fillet 162. The height of the intermediate section 163 is between 0.50 mm to 2.0 mm. In several specific embodiments, this height is between about 0.65 mm and 0.85 mm.

As illustrated in FIGS. 7 and 8, the height of the encapsulant 160 above the upper metallic surface 128 is adequate to cover the bonding wires 142 (which extend above surface 128 by about 0.35 mm and 0.40 mm). The height of the encapsulant 160 above the bonding wires 142 is between about 0.20 mm and 0.50 mm. In several specific embodiments, the height above the bonding wires 142 is between about 0.32 mm and 0.41 mm.

FIG. 7 includes the frame 170 positioned completely over the upper surface 128 of the substrate 126. The frame 170 may also extend outward beyond the surface 128 as illustrated in FIG. 9. The frame 170 is positioned with the outer side 177 positioned laterally outward from the surface 128 and over the heat sink 120. A material 180 is positioned between the frame 170 and the heat sink 120. The material 180 may be an adhesive for attaching the frame 170 to the heat sink 120 and/or a sealant to prevent leakage of the encapsulant 160.

In one embodiment of a solar cell receiver 100 as illustrated in FIG. 9, the attach media 150 is SYLGARD 577. SYLGARD 577 is also used as an edge treatment around the lower metalized surface 130, and as the material 180 between the frame 170 and the heat sink 120. The interior space 178 of the frame 170 is filled with a material 181. This material 181 may also be positioned around the outer side 177 of the frame 170. In one embodiment, the material 181 is SS-109 silicone.

In another embodiment (not illustrated), the frame 170 is completely positioned over the heat sink 120 and does not extend over the surface 128.

In one embodiment as illustrated in FIG. 9, the inner side 171 of the frame 170 includes an angled section 175 that angles away from the concentrator 106. The angled section 175 extends from an intermediate point along the inner side 171 to the top side 173 of the frame 170. In one specific embodiment, the angle of the side 175 substantially matches the angle of the intermediate side 111 of the concentrator 106. This provides for the sides 175 and 111 to be substantially parallel. The angled section 175 controls the height of the outer fillet 162. The angled section 175 may also control the height of the inner fillet 161. In one embodiment, the height of the inner fillet 161 is the same as the height at the intersection between the inner side 171 and the angled section 175.

The angled section 175 may extend completely around the frame 170, or may be located along just one or more limited sections of the frame 170. In one embodiment, a first angled section 175 extends along a first section of the frame 170 and faces towards a first face of the rectangular concentrator 106, and a second angled section 175 extends along an opposing second section of the frame 170 and faces towards a second face of the rectangular concentrator. The angle of the angled section 175 may be the same along the various sections of the frame 170, or may vary.

The frame 170 may be positioned over one or more components of the solar cell receiver 100. FIG. 6 includes the frame 170 being positioned over the connection terminals 125, 127 (not illustrated in FIG. 4). The frame 170 further includes openings 176 that receive leads 151 that connect with the connection terminals 125, 127. These openings 176 may only extend inward from the outer side 177 and terminate at an interior of the frame 170 away from the inner side 171 to prevent a possible leakage location for the encapsulant 160. The frame 170 may further extend over the bypass diode 124. The bottom side 172 of the frame 170 may include cut-outs that accommodate the various components. In these various embodiments, the inner side 171 of the frame 170 is positioned between the components and the solar cell 102 to provide a surface for the encapsulant 160 and to prevent leaking of the encapsulant.

The frame 170 may be centered around the concentrator 106 and solar cell 102. Alternatively, the frame 170 may be off-center with one section of the frame 170 being closer to the concentrator 106 and the solar cell 102 than another section.

In some embodiments, the central region 174 of the frame 170 is a single section. The encapsulant 160 may be introduced into the central region 174 and then allowed to flow through the region 174 and cover the various components. The central region 174 may also be divided into two or more separate sections. Construction of the solar cell receiver 100 requires that encapsulant 160 be introduced separately into each of the sections.

During assembly, the frame 170 is attached to the substrate 126 and/or heat sink 120. An adhesive may be used for attachment and also to prevent leakage of the encapsulant 160 during later assembly steps.

After attachment of the frame 170, the encapsulant 160, which may be silicone based, is introduced into the interior space 178. The encapsulant 160 has a surface tension that cases increased fillet heights at the outer edges. After introduction, the encapsulant 160 is cured by heat or other suitable process.

The solar cell 102 may be a multijunction III-V device with a number of solar subcells provided in a stacked arrangement. The solar cell 102 may include upper, middle, and lower subcells having band gaps to maximize absorption of the solar energy. One applicable solar cell is disclosed in U.S. application Ser. No. 12/148,553 filed on Apr. 18, 2008, which is herein incorporated by reference in its entirety.

The bracket 116 (FIG. 3) may extend over the frame 170 with the fasteners 122 attaching to the heat sink 120 at points outside of the frame 170. A lower side of the bracket 116 may contact against or be above the top side 173 of the frame 170. Alternatively, the bracket 116 may be positioned within the central region 174 of the frame 170.

In various implementations described herein, a triple-junction III-V compound semiconductor solar cell is employed, but other types of solar cells could be used depending upon the application. The solar cells 102 may be made from, e.g., silicon (including amorphous, nanocrystalline, or protocrystalline), cadmium telluride, CIGS (copper indium gallium diselenide), CIS (chalcopyrite films of copper indium selenide (CuInSe₂)), gallium arsenide (e.g., GaAs multijunctions), light absorbing dyes (e.g., ruthenium metalorganic dye), or organic semiconductors (e.g., polyphenylene vinylene, copper phthalocyanine or carbon fullerenes).

Since a single solar cell module 200 may not produce sufficient electricity for a given application, two or more solar cell modules 200 may be grouped together into an array. These arrays are sometimes referred to as “panels” or “solar panels.”

While particular embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that, based upon the teachings herein, changes and modifications may be made without departing from this invention and its broader aspects and, therefore, the appended claims are to encompass within their scope all such changes and modifications as are within the scope of this invention. Furthermore, it is to be understood that the invention is solely defined by the appended claims.

It will be understood by those within the art that, in general, terms used herein, and especially in the appended claims (e.g., bodies of the appended claims) are generally intended as “open” terms (e.g., the term “including” should be interpreted as “including but not limited to,” the term “having” should be interpreted as “having at least,” the term “includes” should be interpreted as “includes but is not limited to,” “comprise” and variations thereof, such as, “comprises” and “comprising” are to be construed in an open, inclusive sense, that is as “including, but not limited to,” etc.). It will be further understood by those within the art that if a specific number of an introduced claim recitation is intended, such an intent will be explicitly recited in the claim, and in the absence of such recitation no such intent is present. For example, as an aid to understanding, the following appended claims may contain usage of the introductory phrases “at least one” and “one or more” to introduce claim recitations. However, the use of such phrases should not be construed to imply that the introduction of a claim recitation by the indefinite articles “a” or “an” limits any particular claim containing such introduced claim recitation to inventions containing only one such recitation, even when the same claim includes the introductory phrases “one or more” or “at least one” and indefinite articles such as “a” or “an” (e.g., “a” and/or “an” should typically be interpreted to mean “at least one” or “one or more”); the same holds true for the use of definite articles used to introduce claim recitations. In addition, even if a specific number of an introduced claim recitation is explicitly recited, those skilled in the art will recognize that such recitation should typically be interpreted to mean at least the recited number (e.g., the bare recitation of “two recitations,” without other modifiers, typically means at least two recitations, or two or more recitations). 

1. A solar cell receiver for use in a concentrating solar system which concentrates the solar energy onto a solar cell for converting solar energy to electricity, comprising: a support; a solar cell mounted on the support and comprising one or more III-V compound semiconductor layers; an optical element positioned over the solar cell on an opposite side from the support, the optical element defining an optical channel and including an enlarged inlet that faces away from the solar cell and a reduced outlet that faces towards the solar cell; a frame positioned over the support and having a height above the support that is greater than the solar cell, the frame extending around and enclosing the solar cell in an interior space; and an encapsulant contained within the interior space between the optical element and the frame and covering portions of the support and the solar cell, the encapsulant having an enlarged fillet height at each of the optical element and the frame.
 2. The solar cell receiver of claim 1, wherein the fillet height is in a range of between about 1.0 mm to 3.0 mm and an intermediate section of the encapsulant has a height in a range of between about 0.50 mm to 1.0 mm.
 3. The solar cell receiver of claim 2, wherein the fillet height at the optical element is different than the fillet height at the frame.
 4. The solar cell receiver of claim 1, further comprising first and second electrical terminals mounted on the support and forming anode and cathode connections each with receptacles to couple to adjacent solar cell receivers, the first and second electrical contacts being covered by the frame.
 5. The solar cell receiver of claim 1, wherein the optical element has a tapered shape with the inlet including a larger cross-sectional area than the outlet.
 6. The solar cell receiver of claim 5, wherein an inner side of the frame that faces towards the optical element includes a tapered shape that angles in a common direction as the optical element.
 7. The solar cell receiver of claim 1, further comprising bonding wires that extend between the solar cell and the support, the bonding wires being completely covered by the encapsulant.
 8. The solar cell receiver of claim 7, wherein the encapsulant covers the bonding wires and extends above the bonding wires by a height in a range of between about 0.20 mm to 0.50 mm.
 9. The solar cell receiver of claim 1, wherein the support is a ceramic substrate having first and second opposed metalized surfaces with the encapsulant directly contacting against the first metalized surface.
 10. The solar cell receiver of claim 1, further comprising a transparent adhesive disposed between the optical element and the solar cell, the transparent adhesive preventing the encapsulant from being positioned between the optical element and the solar cell.
 11. A solar cell receiver for use in a concentrating solar system which concentrates the solar energy onto a solar cell for converting solar energy to electricity, comprising: a support; a solar cell mounted on the support and comprising one or more III-V compound semiconductor layers; an optical element positioned over the solar cell and having an optical channel with an inlet that faces away from the solar cell and an outlet that faces towards the solar cell; a frame positioned over the support and extending around the solar cell, the frame having an inner side that extends above the support and faces towards the optical element with the inner side being positioned between 2.0 mm to 5.0 mm away from the optical element; and an encapsulant positioned over the support and contained between the optical element and the frame, the encapsulant having enlarged heights at contact points with the optical element and the frame of between about 1.0 mm to 3.0 mm and a reduced height between the contact points away from the optical element and the frame.
 12. The solar cell receiver of claim 11, further comprising bonding wires that extend outward from the solar cell and are positioned above the support, the encapsulant covering the bonding wires.
 13. The solar cell receiver of claim 11, wherein the frame includes a hollow interior that is filled with a material to prevent leakage of the encapsulant.
 14. The solar cell receiver of claim 11, wherein the frame extends over a connection terminal that is mounted to and extends upward above the support.
 15. The solar cell receiver of claim 11, wherein the support is mounted on a heat sink and at least a portion of the frame is positioned directly over the heat sink and away from the support.
 16. The solar cell receiver of claim 11, wherein each of the inner side of the frame and the support are substantially flat with the inner side being perpendicular to the support.
 17. A method of making a solar cell receiver, comprising: mounting a solar cell on a support with the solar cell comprising one or more III-V compound semiconductor layers; mounting bond wires between the solar cell and the support; mounting an optical element defining an optical channel over the solar cell so that the solar cell is in the optical path of the optical channel; mounting a frame on the support that surrounds the solar cell and defines an enclosed interior space between the frame and the optical element; introducing a fluid encapsulant in the enclosed interior space between the frame and the optical element and encapsulating at least a portion of the solar cell, the bond wires, and at least a portion of the optical element, the fluid encapsulant having an increased surface tension and forming enlarged fillets at the optical element and the frame and a reduced intermediate section with the fillets having a greater height above the support than the intermediate section; and curing the fluid encapsulant.
 18. The method of claim 17, further comprising positioning the frame over a connection terminal that is mounted on support with the frame completely surrounding the connection terminal.
 19. The method of claim 17, further comprising applying a sealant around an exterior of the frame and preventing the encapsulant from leaking from the enclosed interior space.
 20. The method of claim 17, further comprising attaching a secondary optical element to the support and over the optical element with a bracket that extends over a top side of the frame.
 21. A solar cell module to convert light to electricity comprising: a housing with a plurality of lenses that form an enclosed interior space; a plurality of solar cell receivers connected to the housing and spaced away from the plurality of lenses, each of the plurality of solar cell receivers comprising: a ceramic substrate having a first metalized surface and an opposing second metalized surface, the first metalized surface having separate conductive regions; a III-V compound semiconductor multijunction solar cell having an anode terminal electrically connected to a first one of the conductive regions of the ceramic substrate and a cathode terminal electrically connected to a second one of the conductive regions; a bypass diode connected across the first and second conductive regions of the ceramic substrate in parallel with the solar cell; a first optical element positioned above the solar cell and including a tapered shape with a larger inlet that faces away from the solar cell and a smaller outlet that faces towards the solar cell; a second optical element positioned above the solar cell; a frame positioned over the ceramic substrate and having a height above the ceramic substrate that is greater than the solar cell, the frame extending around and enclosing the solar cell in an interior space; and an encapsulant contained within the interior space between the second optical element and the frame and covering portions of the ceramic substrate and the solar cell, the encapsulant having an enlarged fillet height at each of the second optical element and the frame; each of said solar cell receivers, first optical elements, and second optical elements being disposed in an optical path of one of the plurality of lenses, wherein the lens, the first optical element, and the second optical element concentrate the light onto the respective solar cell by a factor of 1000 or more to generate in excess of 25 watts of peak power. 